{"id":"F2006B03325","name":"AD/B767/149 - Passenger Entertainment System FAA STC ST09022AC-D","slug":"ad-b767-149-passenger-entertainment-system-faa-stc-st09022ac-d","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"in_force","isInForce":true,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":42762,"registerId":"commonwealth-F2006B03325-current","compilationNumber":null,"startDate":"2026-04-01","status":"InForce","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/B767/149 - Passenger Entertainment System FAA STC ST09022AC-D","content":"COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 \\- 105 CIVIL AVIATION SAFETY AUTHORITY\n\nSCHEDULE OF AIRWORTHINESS DIRECTIVES\n\n![](image.001.png)  \n![](image.002.png)  \nBoeing 767 Series Aeroplanes\n\nAIRWORTHINESS DIRECTIVE\n\n![](image.002.png)\n\n![](image.002.png)  \nFor the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.\n\nAD/B767/149 Passenger Entertainment System\n\nFAA STC ST09022AC-D\n\n  \n9/2001\n\nApplicability: Model 767-200 series airplanes modified by United States Federal Aviation Administration (FAA) Supplemental Type Certificate (STC) ST09022AC-D.\n\nRequirement: 1. Accomplish the following:\n\n    Modify the passenger entertainment system (PES) to install a load shed relay and associated wiring for the Airshow System portion of the PES, in accordance with Raytheon Service Bulletin 767VIP-24-1, dated 28 August 2000.\n\n    b. Revise the Airplane Operations Manual (AOM) to describe the function of the utility bus power switch located on the flight deck, including the use of this switch to remove power to the PES, in accordance with Raytheon Airplane Operations Manual Supplement 767-27G, dated 18 October 2000.\n\n2. PES may not be installed on any aeroplane in accordance with STC ST09022AC- D, unless it is modified and the AOM is revised in accordance with this Directive.\n\nNote: FAA AD 2001-14-13 Amdt 39-12324 refers.\n\nCompliance: For Requirement 1 \\- Within 18 months after the effective date of this Directive.\n\nFor Requirement 2 \\- As of the effective date of this Directive.\n\nThis Airworthiness Directive becomes effective on 6 September 2001.\n\nCOMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 \\- 105 CIVIL AVIATION SAFETY AUTHORITY\n\nSCHEDULE OF AIRWORTHINESS DIRECTIVES\n\nBackground: This Directive requires the modification of the PES installed by STC ST09022AC-D and the revision of the AOM. This action is required to ensure that, when necessary, the flight crew is able to remove electrical power from the PES and is advised of appropriate procedures for such action. Inability to remove power from the PES during a non-normal or emergency situation could result in inability to control smoke or fumes in the airplane flight deck or cabin.\n\n![Signature of James Coyne, Delegate of the Civil Aviation Safety Authority.](image.003.png)  \n\nJames Coyne\n\nDelegate of the Civil Aviation Safety Authority 23 July 2001\n\n![](image.002.png)  \n\nThe above AD is notified in the Commonwealth of Australia Gazette on 15 August 2001.","sortOrder":0}],"analysis":{"kimi_summary":{"content_quality":"ok","complexity_score":2,"scope_assessment":{"changed":false,"description":"This AD maintains its original narrow scope: addressing a specific unsafe condition in a specific supplemental type certificate installation on a specific aircraft model. There is no evidence of scope creep."},"complexity_factors":["Very short document (approximately 400 words)","Only 2 substantive requirements with clear sub-parts","Single applicability criterion (specific aircraft model + specific modification)","No defined terms section — all technical terms are either self-explanatory or explained in context","No cross-references to other legislation beyond a single 'note' referencing the corresponding FAA directive","Linear structure: Background → Applicability → Requirement → Compliance → Effective date","No conditional logic, exceptions, or nested provisions"],"plain_english_summary":"This CASA Airworthiness Directive applies to Boeing 767-200s modified with the FAA STC ST09022AC-D entertainment/Airshow system. It mandates installing a new electrical relay and wiring to allow a cockpit master switch to remove power, and updating the Airplane Operations Manual with shut‑down procedures. New installations are prohibited unless these fixes are done. It’s intended to ensure pilots can cut power quickly during smoke/fume emergencies; hardware must be fitted within 18 months (effective 6 Sep 2001)."},"flash_summary_failed":{"failed":true,"reason":"A positive credit balance is required for all requests, including BYOK, so fallback providers remain available. Add credits at https://vercel.com/d?to=%2F%5Bteam%5D%2F%7E%2Fai%3Fmodal%3Dtop-up to continue.","source":"analysis-cron"},"flash_summary":{"complexity_score":4,"scope_assessment":{"changed":false,"description":"The AD maintains a narrowly targeted scope: it mandates a specific retrofit and AOM revision for 767-200s modified by STC ST09022AC‑D and prohibits further installations under that STC unless compliant. It does not extend obligations to other aircraft types or unrelated systems."},"complexity_factors":["Technical installation work: fitting a load‑shed relay and associated wiring to the PES (Requirement 1; Raytheon Service Bulletin 767VIP-24-1).","Operational documentation change: revising the Airplane Operations Manual to describe the utility bus power switch and PES power removal (Requirement 1b; Raytheon AOM Supplement 767-27G).","Narrow applicability: applies only to Model 767-200 aeroplanes modified by FAA STC ST09022AC‑D (Applicability) — requires operators to identify affected fleet.","Regulatory constraint on future installs: PES may not be installed under that STC unless the modification and AOM revision are done (Requirement 2), creating an immediate compliance/installation bar.","Fixed compliance deadline: 18 months for retrofit (Compliance) imposes scheduling and resource pressure on operators and maintenance providers.","Cross-reference to FAA AD (Note): coordination with FAA certification/airworthiness action (FAA AD 2001-14-13) may affect parts, instructions, and approvals.","Implementation risk and certification: work likely requires certified technicians and record‑keeping to demonstrate compliance for continued airworthiness.","Relatively low drafting complexity: the AD sets discrete technical and administrative requirements rather than broad regulatory standards."],"plain_english_summary":"This AD requires Boeing 767-200 aeroplanes modified by FAA STC ST09022AC‑D to have their passenger entertainment system fitted with a load‑shed relay and associated wiring, and to update the Airplane Operations Manual to describe the flight‑deck utility bus power switch and how to remove PES power. \n\nAircraft operators and maintenance organisations must perform and pay for the retrofit per Raytheon service documents within 18 months; installations under that STC are prohibited unless the retrofit and manual revision are completed. CASA says the measure ensures crew can remove PES power to help control smoke or fumes."}},"importantCases":[],"_links":{"self":"/api/acts/ad-b767-149-passenger-entertainment-system-faa-stc-st09022ac-d","history":"/api/acts/ad-b767-149-passenger-entertainment-system-faa-stc-st09022ac-d/history","analysis":"/api/acts/ad-b767-149-passenger-entertainment-system-faa-stc-st09022ac-d/analysis","conflicts":"/api/acts/ad-b767-149-passenger-entertainment-system-faa-stc-st09022ac-d/conflicts","importantCases":"/api/acts/ad-b767-149-passenger-entertainment-system-faa-stc-st09022ac-d/important-cases","documents":"/api/acts/ad-b767-149-passenger-entertainment-system-faa-stc-st09022ac-d/documents"}}